Beech 200 accident near Unalaska, Alaska, January 16, 2020
On January 16, 2020 at about 6:06 pm local time, a 1998 Beech 200, registered N547LM, was substantially damaged in an accident during takeoff near Unalaska, Alaska (Unalaska airport). It was flown under charter and air-taxi rules (Part 135). 1 person was seriously injured; 4 others were unhurt. The weather was visual conditions (good weather).
The NTSB's probable cause their words, unchanged
The pilot’s improper decision to takeoff downwind and to load the airplane beyond its allowable gross weight and center of gravity limits, which resulted in an aerodynamic stall and loss of control. Contributing to the accident was the inadequacy of the operator’s safety management system to actively monitor, identify, and mitigate hazards and deficiencies.
Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.
What the record shows
- Date
- January 16, 2020 · about 6:06 pm local time
- Place
- Unalaska, Alaska · Unalaska · map
- Type
- Accident
- Injuries
- 1 person was seriously injured; 4 others were unhurt.
- Weather
- visual conditions (good weather)
- Aircraft
- Beech 200 B200, built 1998 · all 200s on the register
- Registration
- N547LM · no longer on the register · serial BB1642
- Damage
- Substantial damage
- Flight
- Flight · charter and air-taxi rules (Part 135)
The NTSB's narrative final · quoted from the NTSB record
According to the pilot, when the airplane’s airspeed reached about 90 knots during the takeoff roll, he applied back pressure to the control yoke to initiate the takeoff and noted a brief positive rate of climb followed by a sinking sensation. The airspeed rapidly decayed, and the stall warning horn sounded. To correct for the decaying airspeed, he lowered the nose then pulled back on the airplane’s control yoke and leveled the wings just before impacting the ocean. The pilot stated there were no preaccident mechanical malfunctions or anomalies that would have precluded normal operation. Wind about the time of the accident was recorded as 110º downwind of the airplane at 15 knots gusting to 28 knots. The passengers recalled that the pilot’s preflight briefing mentioned the downwind takeoff but included no discussion of the potential effect of the wind conditions on the takeoff. The airplane’s estimated gross weight at the time of the accident was about 769.6 pounds over its approved maximum gross weight, and the airplane’s estimated center of gravity was about 8.24 inches beyond the approved aft limit at its maximum gross weight. It is likely that the pilot’s decision to takeoff downwind and operate the airplane over the maximum gross weight with an aft center of gravity led to the aerodynamic stall during takeoff and loss of control. Downwind takeoffs result in higher groundspeeds and increase takeoff distance. While excessive aircraft weight increases the takeoff distance and stability, and an aft center of gravity decreases controllability. Several instances of the operator’s noncompliance with its operational procedures and risk mitigations were discovered during the investigation, including two overweight flights, inaccurate and missing information on aircraft flight logs, and the accident pilot’s failure to complete a flight risk assessment for the accident flight. The operator had a safety management system (SMS) in place at the time of the accident that required active monitoring of its systems and processes to ensure compliance with internal and external requirements. However, the discrepancies noted with several flights, including the accident flight, indicate that the operator’s SMS program was inadequate to actively monitor, identify, and mitigate hazards and deficiencies.
The complete narrative as the NTSB published it. The NTSB's docket holds the report as a PDF and any photographs, statements and other documents from the investigation.
The factual record from the NTSB's investigation tables, in plain English
What happened, in order
- Stall warn/stick-shaker/pusher during takeoff
- Loss of control in flight during takeoff defining event
- Collision with terrain or object (not controlled flight into terrain) during takeoff
The NTSB's findings
- cause Personnel issues › Task performance › Use of equip/info › Aircraft control › Pilot
- cause Personnel issues › Action/decision › Info processing/decision › Decision making/judgment › Pilot
- cause Aircraft › Aircraft oper/perf/capability › Aircraft capability › Maximum weight › Capability exceeded
- factor Environmental issues › Conditions/weather/phenomena › Wind › Tailwind › Effect on equipment
Pilot
- Certificate: airline transport pilot
- Ratings: multi-engine land; single-engine land; instructor: airplane multi-engine; instructor: airplane single-engine; instrument: airplane
- Flight time: 6,470 hours in all; 756 in this make and model; 14 in the last 90 days; 6 in the last 30 days; 5,850 as pilot in command; 1,750 on instruments
- Last flight review: July 18, 2019
- Medical certificate: Class 1 (without waivers/limitations)
- Seat: left
- Injury: serious injuries
The aircraft
- Airframe total time: 7,058.4 hours
- Last inspection: approved inspection programme, December 5, 2019
- Seats: 8
- Landing gear: retractable
- Engine 1: Pratt & Whitney PT6A-42 (turboprop); 6,867 hours total
- Engine 2: Pratt & Whitney PT6A-42 (turboprop); 7,486 hours total
- Operator: Aero Air
The flight
- Departed from: DUT Dutch Harbor AK
- Destination: Adak AK
- Runway 31, 4,500 ft by 100 ft
Weather at the time
- Light: night
- Wind: from 110° at 15 knots, gusting 28
- Visibility: 8 statute miles
- Sky: overcast at 1,400 ft
- Temperature: 39°F (4°C), dew point 36°F (2°C)
- Altimeter: 29.47 inHg
- Observation at 5:00 pm
Injuries
| Fatal | Serious | Minor | None | |
|---|---|---|---|---|
| Flight crew | 1 | 2 | ||
| Passengers | 2 |
Documents from the investigation the NTSB's docket: the evidence folder behind the report
11 documents, released by the NTSB on March 22, 2022. View them here, or download them; the NTSB redacts some personal details before release, and this site shows the NTSB's own titles rather than its file names.
| # | Document | What it is | |
|---|---|---|---|
| 1 | Weather Study | PDF, 8 pages | View Download |
| 2 | Weather Study - Attachment 1 | PDF, 3 pages | View Download |
| 3 | Cockpit Voice Recorder - Specialista��s Factual Report | PDF, 5 pages | View Download |
| 4 | Pilot/operator Aircraft Accident Report, NTSB Form 6120.1 | PDF, 9 pages | View Download |
| 5 | Witness Statements | PDF, 104 pages | View Download |
| 6 | Memorandum for Record - Safety Management System (SMS) | PDF, 2 pages | View Download |
| 7 | Aircraft Flight Logs | PDF, 2 pages | View Download |
| 8 | Flight Risk Assessment Email | PDF, 1 page | View Download |
| 9 | Weight and Balance | PDF, 3 pages | View Download |
| 10 | Statement of Party Representatives to NTSB Investigation | PDF, 3 pages | View Download |
| 11 | Party Member Submission | PDF, 1 page | View Download |
The same docket at the NTSB · documents without a copy here are fetched from the NTSB when you open them.
Everything on this page comes from the NTSB's public records. The narrative, probable cause and findings are the NTSB's own words; the coded tables behind the report are written out in plain English, with pilots' ages, home towns and medical details left out. The documents and photographs are the NTSB's docket, shown as the NTSB released them. This site's own text never names anyone involved. A preliminary report can change; the final report usually follows one to two years later, and the page is refreshed when it does.
